Entry vehicle performance analysis and atmospheric guidance algorithm for precision landing on Mars
Name
25315321-MIT.pdf
Description
Full printable version
Size
5.39 MB
Format
Adobe PDF
Checksum (MD5)
06fa9cc5c83eae0e1341c341e3a6d344
Author(s)
Dierlam, Todd Allen
Advisor(s)
Richard H. Battin.
Date Issued
1990
Publisher
Massachusetts Institute of Technology
Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990.
Includes bibliographical references (leaves 167-168).
Subjects
Aeronautics and Astronautics
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Terms of Use
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reproduction or distribution in any format is prohibited without written
permission. See provided URL for inquiries about permission.
copyright. They may be viewed from this source for any purpose, but
reproduction or distribution in any format is prohibited without written
permission. See provided URL for inquiries about permission.
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